Revision: 2.3
Date: 10/30/20
F3-2
Section F3 - Flight Test Card - Flight #3
Aircraft Registration:___________
FLIGHT PROCEDURE (continued):
Set altimeter to 29.92 in Hg. Extend flaps to 1/2.
Full throttle climb performance check at 60 kt IAS. Begin filling in table when stabilized at 60 kt
IAS. Airspeed must be held between 58 kt and 62 kt IAS for accurate results. Oil and/or Cylinder
Head temperatures may climb into the caution range. The climb should be terminated if/as
temperatures approach their limits.
NOTE: Data recording for this task can be accomplished by extracting data from EFIS data log.
FULL THROTTLE CLIMB @ 60 kt IAS @ 1/2 flap @ 1050 lb (476.27kg)
pressure altitude
block
time at bottom of alt
block
outside air temp at
middle of alt block
time at top of altitude
block
1,000 ft to 3,000 ft
2,000 ft to 4,000 ft
3,000 ft to 5,000 ft
4,000 ft to 6,000 ft
5,000 ft to 7,000 ft
6,000 ft to 8,000 ft
7,000 ft to 9,000 ft
8,000 ft to 10,000 ft
Stalls:
Power Off w/recovery delayed 3 seconds after break (wings level & ball centered at entry; wings
held level with rudder after break)
Flaps up (Vs)
Verify no unusual flying qualities or other unexpected behavior.
Flaps ½ (Vs1)
Verify no unusual flying qualities or other unexpected behavior.
Flaps full (Vs0)
Verify no unusual flying qualities or other unexpected behavior.
If necessary, climb to no lower than 3,000 ft AGL and establish slow flight at 55 kt zero flaps,
power as required to maintain altitude. Allow airspeed to stabilize. Fly a 4-way speed box and fill
in table.
(Optional: This may be accomplished using the autopilot.)
NOTE: Data recording for this task can be accomplished by extracting data from EFIS data log.
55 kt & ZERO FLAP AIRSPEED CALIBRATION
GPS GRND TRCK
0 deg
90 deg
180 deg
270 deg
DENSITY ALT:
OBSERVED
AIRSPEED (KT)
PRESSURE ALT:
GPS GRND
SPEED (KT)
RPM:
FUEL FLOW
(GAL/HR)
MAP:
Summary of Contents for RV 12iS
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